JP6778147B2 - 複合材料翼及び複合材料翼の製造方法 - Google Patents

複合材料翼及び複合材料翼の製造方法 Download PDF

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Publication number
JP6778147B2
JP6778147B2 JP2017108380A JP2017108380A JP6778147B2 JP 6778147 B2 JP6778147 B2 JP 6778147B2 JP 2017108380 A JP2017108380 A JP 2017108380A JP 2017108380 A JP2017108380 A JP 2017108380A JP 6778147 B2 JP6778147 B2 JP 6778147B2
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JP
Japan
Prior art keywords
laminated body
composite material
wing
material layer
blade
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
JP2017108380A
Other languages
English (en)
Japanese (ja)
Other versions
JP2018204461A5 (zh
JP2018204461A (ja
Inventor
良次 岡部
良次 岡部
野中　吉紀
吉紀 野中
新藤　健太郎
健太郎 新藤
昌美 神谷
昌美 神谷
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP2017108380A priority Critical patent/JP6778147B2/ja
Priority to PCT/JP2018/020780 priority patent/WO2018221597A1/ja
Priority to DE112018002751.1T priority patent/DE112018002751B4/de
Priority to US16/613,305 priority patent/US11066939B2/en
Priority to CN201880031755.4A priority patent/CN110621849B/zh
Publication of JP2018204461A publication Critical patent/JP2018204461A/ja
Publication of JP2018204461A5 publication Critical patent/JP2018204461A5/ja
Application granted granted Critical
Publication of JP6778147B2 publication Critical patent/JP6778147B2/ja
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Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/302—Details of the edges of fibre composites, e.g. edge finishing or means to avoid delamination
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Composite Materials (AREA)
  • General Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Textile Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Moulding By Coating Moulds (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
JP2017108380A 2017-05-31 2017-05-31 複合材料翼及び複合材料翼の製造方法 Active JP6778147B2 (ja)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP2017108380A JP6778147B2 (ja) 2017-05-31 2017-05-31 複合材料翼及び複合材料翼の製造方法
PCT/JP2018/020780 WO2018221597A1 (ja) 2017-05-31 2018-05-30 複合材料翼及び複合材料翼の製造方法
DE112018002751.1T DE112018002751B4 (de) 2017-05-31 2018-05-30 Verbundschaufel und verfahren zum herstellen einer verbundschaufel
US16/613,305 US11066939B2 (en) 2017-05-31 2018-05-30 Composite blade and method for producing composite blade
CN201880031755.4A CN110621849B (zh) 2017-05-31 2018-05-30 复合材料叶片及复合材料叶片的制造方法

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2017108380A JP6778147B2 (ja) 2017-05-31 2017-05-31 複合材料翼及び複合材料翼の製造方法

Publications (3)

Publication Number Publication Date
JP2018204461A JP2018204461A (ja) 2018-12-27
JP2018204461A5 JP2018204461A5 (zh) 2019-12-26
JP6778147B2 true JP6778147B2 (ja) 2020-10-28

Family

ID=64455134

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2017108380A Active JP6778147B2 (ja) 2017-05-31 2017-05-31 複合材料翼及び複合材料翼の製造方法

Country Status (5)

Country Link
US (1) US11066939B2 (zh)
JP (1) JP6778147B2 (zh)
CN (1) CN110621849B (zh)
DE (1) DE112018002751B4 (zh)
WO (1) WO2018221597A1 (zh)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP7236337B2 (ja) * 2019-06-19 2023-03-09 三菱重工業株式会社 複合材翼及び複合材翼の成形方法
KR102076827B1 (ko) 2019-06-28 2020-02-12 국방과학연구소 복합재료를 이용한 일체형 접이식 날개 및 이의 제조 방법
FR3134140A1 (fr) * 2022-04-01 2023-10-06 Safran Renfort pour une aube composite d’une turbomachine, comprenant un mélange de découpes de fibre et d’un tackifiant
FR3134139A1 (fr) * 2022-04-01 2023-10-06 Safran Renfort pour une aube composite d’une turbomachine, comprenant un empilement de plis

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3132841A (en) 1958-05-12 1964-05-12 Gen Motors Corp Compressor blade and manufacture thereof
US4810167A (en) * 1986-12-08 1989-03-07 Hartzell Propeller Inc. Composite aircraft propeller blade
US5375978A (en) 1992-05-01 1994-12-27 General Electric Company Foreign object damage resistant composite blade and manufacture
DE10326719A1 (de) * 2003-06-06 2004-12-23 Rolls-Royce Deutschland Ltd & Co Kg Verdichterschaufelfuß für Triebwerksschaufeln von Flugzeugtriebwerken
US20050158171A1 (en) * 2004-01-15 2005-07-21 General Electric Company Hybrid ceramic matrix composite turbine blades for improved processibility and performance
FR2890126B1 (fr) * 2005-08-26 2010-10-29 Snecma Ensemble et procede pour le montage du pied d'une aube de turbomachine, soufflante, compresseur et turbomachine comportant un tel ensemble
DE102006049818A1 (de) * 2006-10-18 2008-04-24 Rolls-Royce Deutschland Ltd & Co Kg Fanschaufel aus Textilverbundwerkstoff
GB0815482D0 (en) * 2008-08-27 2008-10-01 Rolls Royce Plc A blade and method of making a blade
EP2322763A1 (de) * 2009-11-17 2011-05-18 Siemens Aktiengesellschaft Turbinen- oder Verdichterschaufel
CN102514205B (zh) * 2011-11-10 2016-02-17 洛阳双瑞风电叶片有限公司 一种复合材料风电叶片根部成型方法
US9435209B2 (en) * 2012-10-25 2016-09-06 General Electric Company Turbomachine blade reinforcement
US9370921B2 (en) 2012-11-01 2016-06-21 The Boeing Company Composite radius fillers and methods of forming the same
JP6003660B2 (ja) * 2013-01-11 2016-10-05 株式会社Ihi セラミックス基複合部材
EP3044420A2 (en) * 2013-09-11 2016-07-20 General Electric Company Ply architecture for integral platform and damper retaining features in cmc turbine blades
US9566739B2 (en) * 2014-02-18 2017-02-14 The Boeing Company Composite filler
US9963979B2 (en) * 2014-11-17 2018-05-08 Rolls-Royce North American Technologies Inc. Composite components for gas turbine engines
EP3239469B1 (en) * 2014-11-20 2019-01-09 Rolls-Royce North American Technologies, Inc. Composite blades for gas turbine engines
US10577939B2 (en) * 2016-11-01 2020-03-03 Rolls-Royce Corporation Turbine blade with three-dimensional CMC construction elements

Also Published As

Publication number Publication date
DE112018002751T5 (de) 2020-02-13
DE112018002751B4 (de) 2022-12-08
CN110621849A (zh) 2019-12-27
US20210108521A1 (en) 2021-04-15
WO2018221597A1 (ja) 2018-12-06
US11066939B2 (en) 2021-07-20
CN110621849B (zh) 2021-09-07
JP2018204461A (ja) 2018-12-27

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